REUSABLE LAUNCH VEHICLE - SCI & TECH

News: ISRO successfully conducts landing experiment of the Reusable Launch Vehicle

 

What's in the news?

       The Indian Space Research Organization has successfully carried out the landing experiment of the Reusable Launch Vehicle-Technology Demonstration (RLV-TD) programme at the Aeronautical Test Range in Challakere, Chitradurga.

 

Key takeaways:

       An Indian Air Force Chinook helicopter was used to drop the RLV-TD from a 4.5-km altitude and ISRO executed the landing experiment as planned.

       The Reusable Launch Vehicle Autonomous Landing Mission (RLV LEX) test was the second of five tests.

       The experiment was carried out nearly seven years after the technology demonstration of an RLV and the first experiment was conducted successfully by ISRO on May 23, 2016, on the RLV-TD (HEX) mission.

 

ISRO’s RLV TD project:

       ISRO aims to develop RLVs, or space planes/shuttles, which can travel to low earth orbits to deliver payloads and return to earth for use again.

 

Objective:

       To develop essential technologies for a fully reusable launch vehicle to enable low-cost access to space.

 

Mission:

       The RLV-TD will be used to develop technologies like hypersonic flight (HEX), autonomous landing (LEX), return flight experiment (REX), powered cruise flight, and Scramjet Propulsion Experiment (SPEX).

 

Features:

       ISRO’s RLV-TD looks like an aircraft. It consists of a fuselage, a nose cap, double delta wings, and twin vertical tails.

       The 2016 experiment involved sending a winged spacecraft on a rocket powered by a conventional solid booster (HS9) engine used by ISRO into space. The spacecraft traveled at a speed of Mach 5 (five times the speed of sound) when re-entering the earth’s orbit and traveled a distance of 450 km before splashdown in the Bay of Bengal.

 

Significance:

       With the costs acting as a major deterrent to space exploration, a reusable launch vehicle is considered a low-cost, reliable, and on-demand mode of accessing space.

       Nearly 80 to 87 percent of the cost in a space launch vehicle goes into the structure of the vehicle. The costs of propellants are minimal in comparison. By using RLVs the cost of a launch can be reduced by nearly 80 percent of the present cost.

 

Go back to basics:

First Experiment:

       In the first flight, critical technologies such as autonomous navigation, guidance and control, reusable thermal protection system, and re-entry mission management have been successfully validated.

 

Second Experiment:

       In the second flight, autonomous landing under the exact conditions of a Space Re-entry vehicle’s landing - high speed, unmanned, precise landing from the same return path were tested.

       It also tested landing parameters such as ground relative velocity, the sink rate of landing gears, and precise body rates, as might be experienced by an orbital re-entry space vehicle in its return path, were achieved.

 

Difference between first and second experiment:

       According to ISRO, the first test with RLV-TD (HEX1) involved the vehicle landing on a hypothetical runway over the Bay of Bengal while the LEX experiment conducted recently involved a precise landing on a runway.

 

Three more experiments - Return flight experiment (REX), powered cruise flight, and Scramjet Propulsion Experiment (SPEX) have to be conducted.